Patents by Inventor Michael L. Fortner

Michael L. Fortner has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 8307767
    Abstract: An initiator includes a detonation port and a reactive panel coupled with the detonation port. The reactive panel includes an inner panel, an outer panel, and an explosive sheet disposed between the inner panel and the outer panel and operatively associated with a venting device. A system for venting a container includes a venting device and an initiator coupled with the venting device. The initiator includes a detonation port and a reactive panel coupled with the detonation port. The reactive panel includes an inner panel, an outer panel, and an explosive sheet disposed between the inner panel and the outer panel and operatively associated with the venting device. A method of venting a container includes providing a venting system operatively associated with a container, detonating an explosive sheet of the venting system, and venting the container as a result of detonating the explosive sheet.
    Type: Grant
    Filed: May 2, 2005
    Date of Patent: November 13, 2012
    Assignee: Lockheed Martin Corporation
    Inventors: Anthony T. Skinner, Michael L. Fortner
  • Patent number: 8136450
    Abstract: An apparatus includes a heat-to-detonation transition manifold, a heat pipe connected to the transition manifold, a linear shaped charge, and a transfer line connecting the heat-to-detonation transition manifold and the linear shaped charge. An apparatus includes a thermally-activated pyrotechnic train and a linear shaped charge coupled with the pyrotechnic train. A method includes initiating a deflagrating material at a predetermined temperature or within a predetermined range of temperatures, initiating a detonating material with the deflagrating material, and initiating a linear shaped charge with the detonated material.
    Type: Grant
    Filed: March 30, 2009
    Date of Patent: March 20, 2012
    Assignee: Lockheed Martin Corporation
    Inventors: Anthony T. Skinner, Michael L. Fortner, Marcus J. Dill, David N. Zichichi, Lamar R. Lunsford
  • Publication number: 20110113950
    Abstract: A composite material suitable for use as an armor includes a first layer of a metallic material and a second layer, metallurgically bonded with the first layer. The second layer includes a matrix of the material of the first layer and a plurality of brittle particles dispersed in the matrix. A method for making a composite structure suitable for use as an armor from a workpiece of a metallic material includes the steps of plasticizing a fractional thickness of the workpiece using a friction stir process, introducing a plurality of brittle particles into the plasticized, fractional thickness of the workpiece, and dispersing the plurality of brittle particles into the plasticized, fractional thickness of the workpiece using the friction stir process.
    Type: Application
    Filed: January 10, 2006
    Publication date: May 19, 2011
    Inventors: Charles K. Reed, David L. Hunn, Michael L. Fortner
  • Publication number: 20090183648
    Abstract: An apparatus includes a heat-to-detonation transition manifold, a heat pipe connected to the transition manifold, a linear shaped charge, and a transfer line connecting the heat-to-detonation transition manifold and the linear shaped charge. An apparatus includes a thermally-activated pyrotechnic train and a linear shaped charge coupled with the pyrotechnic train. A method includes initiating a deflagrating material at a predetermined temperature or within a predetermined range of temperatures, initiating a detonating material with the deflagrating material, and initiating a linear shaped charge with the detonated material.
    Type: Application
    Filed: March 30, 2009
    Publication date: July 23, 2009
    Applicant: Lockheed Martin Corporation
    Inventors: Anthony T. Skinner, Michael L. Fortner, Marcus J. Dill, David N. Zichichi, Lamar R. Lunsford
  • Patent number: 7530314
    Abstract: An apparatus includes a thermally-activated, deflagration initiation device, a deflagration-to-detonation transition manifold, a first transfer line connecting the deflagration initiation device and the deflagration-to-detonation transition manifold, and a linear shaped charge coupled with the first transfer line. An apparatus includes a heat-to-detonation transition manifold, a heat pipe connected to the transition manifold, a linear shaped charge, and a transfer line connecting the heat-to-detonation transition manifold and the linear shaped charge. An apparatus includes a thermally-activated pyrotechnic train and a linear shaped charge coupled with the pyrotechnic train. A method includes initiating a deflagrating material at a predetermined temperature or within a predetermined range of temperatures, initiating a detonating material with the deflagrating material, and initiating a linear shaped charge with the detonated material.
    Type: Grant
    Filed: May 13, 2005
    Date of Patent: May 12, 2009
    Assignee: Lockheed Martin Corporation
    Inventors: Anthony T. Skinner, Michael L. Fortner, Marcus J. Dill, David N. Zichichi, Lamar R. Lunsford
  • Patent number: 6845718
    Abstract: A projectile includes a body, a penetrator disposed at least partially within the body for penetrating a target or barrier, and means for propelling the penetrator from the body. A method includes directing a projectile toward a target or barrier and propelling a penetrator from within a body of the projectile. An apparatus for propelling a penetrator from a projectile includes a high energy power source and means for guiding the penetrator from the projectile.
    Type: Grant
    Filed: December 18, 2002
    Date of Patent: January 25, 2005
    Assignee: Lockheed Martin Corporation
    Inventors: Michael L. Fortner, Carl G. Baldwin
  • Publication number: 20040118312
    Abstract: A projectile includes a body, a penetrator disposed at least partially within the body for penetrating a target or barrier, and means for propelling the penetrator from the body. A method includes directing a projectile toward a target or barrier and propelling a penetrator from within a body of the projectile. An apparatus for propelling a penetrator from a projectile includes a high energy power source and means for guiding the penetrator from the projectile.
    Type: Application
    Filed: December 18, 2002
    Publication date: June 24, 2004
    Inventors: Michael L. Fortner, Carl G. Baldwin
  • Publication number: 20030177933
    Abstract: A penetrator includes a shaped charge warhead defining a bore therethrough, an augmenting warhead disposed within the bore, and a detonating mechanism coupled with and capable of detonating the shaped charge warhead and the augmenting warhead. A projectile includes a shaped charge warhead defining a bore therethrough being disposed within the projectile, an augmenting warhead disposed within the bore, and a detonating mechanism disposed within the projectile and being coupled with and capable of detonating the shaped charge warhead and the augmenting warhead. A method includes at least partially perforating the barrier to form a slug and dislodging the slug from the barrier.
    Type: Application
    Filed: March 20, 2002
    Publication date: September 25, 2003
    Inventors: Michael L. Fortner, Warren B. Estes